Aerodynamic characteristics in sideslip of wing-fuselage combinations; wings have sweep angle of 45° at quarter-chord line, aspect ratio of 4, taper ratios of 0.3, 0.6, and 1.0, and NACA 65A006 airfoil section.
Wind-tunnel investigation of static lateral stability characteristics of wing-fuselage combinations at high subsonic speeds -- Taper-ratio series
NACA -- Tech Note
1957
25 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.